This document addresses the key challenges relevant the application of electromechanical actuators for Load Control and Alleviation purposes on secondary flight control surfaces. In the framework of Regional Aircraft IADP research program Leonardo and ASTIB, Core Partners in the research project, are developing technologies aimed to reach a TRL6 level. The starting point for the work has been the development of relevant technologies achieved in the Clean Sky GRA ITD. These technologies are being further developed with the aim to achieve much higher integration and validation levels. The design of flight control architecture involves several critical aspects. EMA’s and high voltage have long been used for aerospace applications; the innovation is their application for new or critical functions such load control and alleviation considering the strong constraints in terms of closed loop response, stability, space envelope, mass, efficiency and technological maturity. In this paper are summarized the results and criticalities for the three major areas of interest : architectural design, EMA’s design and PHM functions.

Electrical Flight Control for Load Control and Alleviation System / Pozzuto, Giuseppe; DE MARTIN, Andrea; Pispola, Giuseppe; Palmieri, Massimo; Gallorin, Federico. - (2019). ((Intervento presentato al convegno More Electric Aircraft 2019 tenutosi a Tolouse (FRA) nel 6-7 February.

Electrical Flight Control for Load Control and Alleviation System

Andrea De Martin;
2019

Abstract

This document addresses the key challenges relevant the application of electromechanical actuators for Load Control and Alleviation purposes on secondary flight control surfaces. In the framework of Regional Aircraft IADP research program Leonardo and ASTIB, Core Partners in the research project, are developing technologies aimed to reach a TRL6 level. The starting point for the work has been the development of relevant technologies achieved in the Clean Sky GRA ITD. These technologies are being further developed with the aim to achieve much higher integration and validation levels. The design of flight control architecture involves several critical aspects. EMA’s and high voltage have long been used for aerospace applications; the innovation is their application for new or critical functions such load control and alleviation considering the strong constraints in terms of closed loop response, stability, space envelope, mass, efficiency and technological maturity. In this paper are summarized the results and criticalities for the three major areas of interest : architectural design, EMA’s design and PHM functions.
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Utilizza questo identificativo per citare o creare un link a questo documento: http://hdl.handle.net/11583/2728858
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